PERFORMANCE SPECIFICATION LUBRICATING OIL, HELICOPTER TRANSMISSION SYSTEM, SYNTHETIC BASE, NATO CODE NUMBER: O-165

Size: px
Start display at page:

Download "PERFORMANCE SPECIFICATION LUBRICATING OIL, HELICOPTER TRANSMISSION SYSTEM, SYNTHETIC BASE, NATO CODE NUMBER: O-165"

Transcription

1 METRIC 7 October SCOPE PERFORMANCE SPECIFICATION LUBRICATING OIL, HELICOPTER TRANSMISSION SYSTEM, SYNTHETIC BASE, NATO CODE NUMBER: O-165 This specification is approved for use by all Departments and Agencies of the Department of Defense. 1.1 Scope. This specification covers the requirements for one grade of a synthetic base helicopter transmission system lubricating oil, which has a nominal viscosity of 9 mm²/s at 100 C and which is typically made with neopentyl polyol ester base stocks. This oil is identified by NATO Code Number O APPLICABLE DOCUMENTS.1 General. The documents listed in this section are specified in sections 3 and 4 of this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements cited in sections 3 and 4 of this specification, whether or not they are listed. Comments, suggestions, or questions on this document should be addressed to: Commander, Naval Air Warfare Center, Aircraft Division Lakehurst, Code 4.1., Mail Stop 10-3, Route 547, Joint Base MDL, NJ or ed to michael.sikora@navy.mil. Since contact information can change, you may want to verify the currency of this address information using the ASSIST Online database at AMSC N/A FSC 9150

2 . Government documents...1 Specifications and standards. The following specifications and standards form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. FEDERAL STANDARD FED-STD Testing Method of Lubricants, Liquid Fuels, and Related Products DEPARTMENT OF DEFENSE SPECIFICATIONS MIL-PRF Lubricating Oil, Aircraft Turbine Engine, Synthetic Base MIL-PRF Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, NATO Code Numbers O-15, O-154, O-156, and O-167 MIL-DTL DOD-PRF Spectrometric Oil Standards Lubricating Oil, Helicopter Transmission System, Synthetic Base (Copies of these documents are available online at or Other Government documents, drawings, and publications. The following other Government documents, drawings, and publications form a part of this document to the extent specified herein. Unless otherwise specified, the issues are those cited in the solicitation or contract. DEPARTMENT OF DEFENSE TECHNICAL MANUAL DEPARTMENT OF THE NAVY NAVAIR Joint Oil Analysis Program Manual Volume II, Spectrometric and Physical Test Laboratory Operating Requirements and Procedures. (Copies of this document are available from james.mcdonnell@navy.mil or the Naval Air Systems Command, Navy Oil Analysis Program, 9 Elmer Road, Building 360, Unit 4, Patuxent River, MD )

3 .3 Non-Government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. ASTM INTERNATIONAL ASTM D9 - Standard Test Method for Flash and Fire Points by Cleveland Open Cup Tester ASTM D97 - Standard Test Method for Pour Point of Petroleum Products ASTM D445 - Standard Test Method for Kinematic Viscosity of Transparent and Opaque Liquids (and Calculation of Dynamic Viscosity) ASTM D89 - Standard Test Method for Foaming Characteristics of Lubricating Oils ASTM D97 - Standard Test Method for Evaporation Loss of Lubricating Greases and Oils ASTM D53 - Standard Test Method for Viscosity and Viscosity Change After Standing at Low Temperature of Aircraft Turbine Lubricants ASTM D603 - Standard Test Method for Sonic Shear Stability of Polymer-Containing Oils ASTM D347 - Standard Test Method for Air Release Properties of Petroleum Oils ASTM D Standard Practice for Manual Sampling of Petroleum and Petroleum Products ASTM D Standard Practice for Automatic Sampling of Petroleum and Petroleum Products ASTM D Standard Test Method for Corrosiveness and Oxidation Stability of Hydraulic Oils, Aircraft Turbine Engine Lubricants, and Other Highly Refined Oils ASTM D Standard Test Method for Multielement Determination of Used and Unused Lubricating Oils and Base Oils by Inductively Coupled Plasma Atomic Emission Spectrometry (ICP-AES) ASTM D Standard Test Method for Pour Point of Petroleum Products (Automatic Pressure Pulsing Method) ASTM D Standard Test Method for Pour Point of Petroleum Products (Automatic Tilt Method) ASTM D Standard Test Method for Pour Point of Petroleum Products (Rotational Method) ASTM D Standard Test Method for Determination of Wear Metals and Contaminants in Used Lubricating Oils or Used Hydraulic Fluids by Rotating Disc Electrode Atomic Emission Spectrometry (Copies of these documents are available from 3

4 AMERICAN SOCIETY FOR QUALITY (ASQ) ANSI/ASQ Z1.4 - Sampling Procedures and Tables for Inspection by Attributes (Copies of this document are available from NATIONAL TOXICOLOGY PROGRAM Annual Report on Carcinogens (Copies of this document are available from SOCIETY OF AEROSPACE ENGINEERS (SAE) INTERNATIONAL AEROSPACE MATERIAL SPECIFICATIONS (AMS) SAE AMS317/1 - Test Slabs, Acrylonitrile butadiene (NBr-H), Medium-High Acrylonitrile, SAE AMS317/4 - Test Slabs, Fluoroelastomer (FKM), AEROSPACE RECOMMENDED PRACTICE (ARP) SAE ARP Test Method for the Determination of Total Acidity in Polyol Ester and Diester Gas Turbine Lubricants by Automatic Potentiometric Titration (Copies of these documents are available from Order of precedence. Unless otherwise noted herein or in the contract, in the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 4

5 3. REQUIREMENTS 3.1 Qualification. The lubricating oil furnished under this specification shall be a product that is authorized by the qualifying activity for listing on the applicable qualified products list before contract award (see 4., 6.3, 6.4, and 6.5). 3. Materials. The composition of the lubricating oil is not limited; however, materials containing barium, organic compounds of titanium, and known or suspected human carcinogens (as defined by the National Toxicology Program s Annual Report on Carcinogens) are prohibited. Recycled basestocks are permitted; however, each batch shall be fully tested in accordance with the qualification requirements of this specification. If a tricresyl phosphate (TCP) additive is used, the TCP additive shall not contain more than 0. percent by weight of ortho cresol containing isomers of tricresyl phosphate. The manufacturer may be required to submit certification of conformance to this section (see 6.) Acid assay. The acid components, in mole-percent, of the finished oil submitted as the qualification test sample, and noted on batch conformance reports, shall be determined in accordance with FED-STD-791, method 3500 or other equivalent gas chromatography methods as determined by the qualifying activity. The manufacturer may then select a range of 10 mole-percent for each acid component to bracket the values measured on the qualification sample by the qualifying laboratory. The major acid components (10 mole-percent or greater) of production lots of oil shall fall within the stated range for each acid. The minor acid components shall not exceed 10 total mole-percent in bulk lots. a. Alternate methods may be used if approved by the qualifying activity; however, only FED-STD-791, method 3500, shall be used for referee tests. 3.3 Chemical and physical requirements. The lubricating oil shall conform to the requirements specified in table I. 5

6 TABLE I. Physical, chemical, and performance requirements. Characteristic Requirement Test Method Test Reference Paragraph Acid assay Report (see 3..1) FED-STD-791, Method 3500 Low Temperature Viscosity, mm²/s, ASTM D53 at -3 C (-5 F), maximum 13,000 Percent change after 7 hours at -3 C (-5 F), maximum ± Viscosity, mm²/s, ASTM D445 at 100 C (1 F) at 40 C (104 F), minimum 48 Flash point, minimum 3 C ASTM D9 (450 F) Pour point, maximum -40 C (-40 F) ASTM D97 or ASTM D5950 ASTM D5985 ASTM D5949 Total acid number, mg KOH/g, maximum 1.5 SAE ARP5088 Evaporation loss, percent by weight, 6.5 ASTM D hours at 04 C (400 F), maximum 5.0 Foaming, foam volume, ml, maximum ASTM D89 5 minutes aeration at 4 C (75 F) 5 1 minute settling at 4 C (75 F) none 5 minutes aeration at 93.5 C (00 F) 5 1 minute settling at 93.5 C (00 F) none 5 minutes aeration at 4 C (75 F) (after 5 test at 93.5 C, above) 1 minute settling at 4 C (75 F) none Rubber compatibility Rubber swell, percent increase SAE AMS317/1, 7 hours at 70 C (158 F) SAE AMS317/4, 7 hours at 04 C (400 F) Standard silicone rubber, 96 hours at 11 C (50 F) FED-STD-791 Method 3604 Tensile strength loss, percent, max Standard silicone rubber, 96 hours at 11 C (50 F) 80 Method

7 TABLE I. Physical, chemical, and performance requirements - Continued. Characteristic Requirement Test Method Test Reference Paragraph Compatibility Turbidity Compatible None FED-STD-791 Method Sediment, mg/l, maximum 10.0 Air release value at 50 C (1 F), 3.3 minutes ASTM D347 maximum Low temperature Storage Stability, 6 weeks at -18 C (0 F) Stability testing of first production run Sediment Visual undissolved water Sediment through 1. micron filter, maximum Total ash content, maximum Shear stability, viscosity loss at 40 C (104 F), maximum Trace metal content by RDE-AES, mg/kg (ppm by weight), maximum Aluminum (Al) Iron (Fe) Chromium (Cr) Silver (Ag) Copper (Cu) Tin (Sn) Magnesium (Mg) Nickel (Ni) Titanium (Ti) Silicon (Si) Zinc (Zn) Lead (Pb) Molybdenum (Mo) Boron (B) No crystallization, separation or gelling Meet conformance inspection tests none 10 mg/l FED-STD- 791, Method mg/l 4 percent ASTM D ASTM D

8 TABLE I. Physical, chemical, and performance requirements - Continued. Characteristic Requirement Test Method Test Reference Paragraph ASTM D Trace metal content by ICP-AES, mg/kg (ppm by weight), maximum Aluminum (Al) Iron (Fe) Chromium (Cr) Silver (Ag) Copper (Cu) Tin (Sn) Magnesium (Mg) Nickel (Ni) Titanium (Ti) Silicon (Si) Zinc (Zn) Lead (Pb) Molybdenum (Mo) Boron (B) Corrosion and oxidative stability a) 7 hours at 150 C (30 F) Viscosity at 40 C (104 F), percent change Total acid number change, maximum Metal weight chg, mg/cm, maximum Steel Silver (Ag) Aluminum (Al) Magnesium (Mg) Copper (Cu) -5 to ±0. ±0. ±0. ±0. ±0.4 ASTM D4636, Alternate Procedure Sludge content (filtered through 10 µm), mg/100 ml of oil, maximum 50 8

9 TABLE I. Physical, chemical, and performance requirements - Continued. Characteristic Requirement Test Method Test Reference Paragraph Corrosion and oxidative stability ASTM D4636, Alternate b) 7 hours at 175 C (347 F) Procedure Viscosity at 40 C (104 F), percent change Total acid number change, maximum -5 to Metal weight chg, mg/cm, maximum Steel ±0. Silver (Ag) ±0. Aluminum (Al) ±0. Magnesium (Mg) ±0. Copper (Cu) ±0.4 Sludge content, (filtered through 10 µm), mg/100 ml oil, maximum Corrosion and oxidative stability c) 7 hours at 04 C (400 F) Viscosity at 40 C (104 F), percent change, maximum Total acid number change, maximum Metal weight chg, mg/cm, maximum Steel Silver (Ag) Aluminum (Al) Magnesium (Mg) Copper (Cu) ±0. ±0. ±0. ±0. ±0.4 ASTM D4636, Alternate Procedure Sludge content (filtered through 10 µm), mg/100 ml oil, maximum 50 9

10 3.4 Bench performance requirements. Bench performance requirements shall be as specified in table II. TABLE II. Bench performance requirements. Characteristic Requirement Test Method Test Reference Paragraph Gear load carrying ability, Relative Rating as % Hercolube A average of 6 determinations minimum 190% FED-STD-791, Method Bearing corrosion, percentage of test samples with no corrosion on raceway, minimum 50% Pass Appendix A Toxicity. The lubricating oil shall have no adverse effect on the health of personnel when used for its intended purpose (see 6.8). 4. VERIFICATION 4.1 Classification of inspections. The inspection and testing of lubricating oil shall be classified as follows: a. Qualification inspection (see 4.). b. Conformance inspection (see 4.3). 4. Qualification inspection. Qualification inspection shall consist of testing to all of the requirements specified in this specification. When required by the qualifying activity, additional flight test service evaluations may be required on candidate formulations (see 4..1) Service evaluation. When candidate lubricants that were the result of unique or unusual formulation or manufacturing technologies are submitted for qualification testing, the qualifying activity (see 4.) may require additional flight test evaluations. The additional evaluations shall be conducted by the qualifying activity, or its designated representative, and shall consist of the following: a. Model type test. A 150-hour, test cell operated, evaluation shall be conducted on a minimum of two different models of helicopter main transmissions used by the US Military. 10

11 b. Flight evaluation. A 500-hour flight evaluation shall be conducted in a Government owned aircraft having the same main transmission model as used in the Model type test above Evaluation criteria. The rating criteria for both the model type test and the flight evaluation will be reported as satisfactory or unsatisfactory. The satisfactory rating is contingent upon the successful completion of the test duration without a lubricant-related discrepancy and the satisfactory condition of the lubricant-wetted parts upon post-test transmission disassembly and inspection. The post-test condition of the candidate lubricant shall be free of deleterious features. 4.. Requalification. Requalification shall be required when any change is made in source of manufacture, purity, or composition of the lubricating oil base stocks or additives (see 6.3.3). A minor change in the oil formulation may be made without requalification testing, but only after notification to, and approval by, the qualifying activity. Two specific requalification categories are reblend and rebrand, outlined in and Reblend lubricating oil. A reblend lubricating oil is an original qualified product, as specified in 4., in which one or more ingredients have been blended by a manufacturer other than the manufacturer of the original formulation. A sample of the reblended lubricating oil shall be subjected to the qualification tests (see 4.). Reblend approvals are initiated by the process specified in Rebrand lubricating oil qualification. A rebrand lubricating oil is a lubricating oil which has successfully passed the qualification tests (see 4.) and is manufactured by the original formulator at the original manufacturing site but is packaged/distributed using a second party identifying trade name. Rebrand approvals are initiated by the process specified in Qualification inspection sample. The qualification test sample shall consist of 08 liters (55 gallons) of finished lubricating oil and 19 liters (5 gallons) of the base oil without additives. A minimum of 100 grams of each additive ingredient used in the manufacture of the qualification test sample shall be submitted prior to qualification (see 6.3.). 4.3 Conformance inspection. Conformance inspection of production lots shall consist of all of the tests specified in table IV. Failure of production lots to pass any of the conformance tests shall be cause for rejection of the lot Manufacturing tolerances. Finished helicopter transmission oils shall be of the same composition and manufactured at the same plants and by the same methods as those used in the qualified formulation Additives. Additives shall be of the same composition and manufactured at the same plants and by the same methods as those used in the qualified formulation. Additive treat rates for each manufactured batch shall not vary from those specified in table III. 11

12 TABLE III. Additive batch concentration tolerances. Nominal Composition of the Approved Material, %wt Range as Percentage of the Nominal Value ±5 >0.1 - < ± ± Basestocks. Basestocks shall be of the same composition and manufactured at the same plants and by the same methods as those used in the qualified formulation. Incidental cross contamination by neopentyl polyol esters other than those used in the original qualification, but suitable by nature and quality for use in aviation helicopter transmission oil applications, shall not exceed 1.0 percent by weight Government lot acceptance. Government lot acceptance testing shall be in accordance with the contract First production lot samples. Stability testing on the first production run shall be performed as outlined in A sample of five cases of 1 quart containers (10 containers) of material from the first production lot supplied to the procuring agency after qualification, and one case of every production lot supplied to the procuring activity thereafter, shall be forwarded to the Naval Air Systems Command, Attn: AIR 4.4.., Propulsion Lubricants Team, 9 Elmer Road, Building 360, Unit 4, Patuxent River, MD

13 TABLE IV. Conformance tests. Characteristic Requirement Test Reference Paragraphs Acid assay Table I Viscosity, mm²/s, Table I at 40 C (104 F) at 100 C (1 F) Flash point, C Table I Pour point, C Table I Total acid number, maximum Table I Evaporation loss, percent by weight Table I 4.4. Foaming, foam volume, ml, maximum Table I Sediment Table I Trace metal content, ppm, maximum Table I Corrosion and oxidative stability 7 hours Table I at 175 C (347 F) Gear load carrying capacity Table II Bearing corrosion Table II Sampling and inspection of oil. Each bulk lot (see 6.9) of material shall be sampled at random in accordance with ASTM D4057 or ASTM D4177 for the conformance inspection tests (see table IV). Inspections shall meet or exceed requirements specified in this specification Conformance test inspection report. The conformance inspection report (see 6.) on each lot of oil shall be provided via electronic means or mailed to the following address: Naval Air Systems Command, Attn: AIR 4.4.., Propulsion Lubricants Team, 9 Elmer Road, Building 360, Unit 4, Patuxent River, MD Examination of filled containers. A random sample of filled containers from each packaged lot (see 6.9), taken in accordance with ANSI/ASQ-Z1.4, shall be examined with regard to fill, closure, sealing and leakage. 4.4 Test methods. All tests shall be performed in accordance with tables I, II, and III Low temperature viscosity. For the purposes of determining the percent viscosity change, the initial viscosity shall be determined 35 ±1 minutes after the viscometer is placed in the bath maintained at -3 ±1.05 C and again at 7 hours ±5 minutes after completion of initial viscosity Evaporation loss. Bath temperature shall be maintained at 04 ±1 C (400 ± F), for the 6.5 hour test period. Air temperature shall be maintained at 04 ±1 C (400 ± F), using a pre-heater, if necessary. 13

14 4.4.3 Rubber compatibility. Standard elastomer stocks shall conform to SAE AMS317/1 and SAE AMS317/ Rubber swell. SAE AMS317/1 and SAE AMS317/4 shall be tested in accordance with FED-STD-791, method Standard Silicone Rubber shall be tested in accordance with FED-STD-791, method Compatibility. The compatibility test shall be performed in accordance with FED-STD-791, method 3403 with the following exception: petroleum ether, with a boiling range of 30 to 60 C, n-heptane, or hexane, shall be used in place of 1,1,1-trichloroethane (O-T-60). Upon completion of the l68 hour oven period, the test flasks shall be stored in the dark at room temperature 4 ±5 C (75 ±10 F) for 1 days before visual inspection for turbidity. Sediment shall be determined in accordance with FED-STD-791, method If the amount of sediment collected after the exposure period is greater than the limit specified in table I additional testing may be performed on the mixture to determine that its performance meets the requirements of this specification. The additional testing may include all of the tests specified in this specification. Referee lubricating oils shall consist of selected oils qualified under this specification, MIL-PRF-3699, MIL-PRF-7808, and DOD-PRF Low temperature storage. Three one quart samples of oil shall be stored in a cold chamber maintained at -18 ±.5 C (0 ±5 F) for 6 weeks. At the end of the storage period, the oil shall be visually inspected for evidence of crystallization, additive separation, and gelling Stability testing of first production run. Five cases of one quart containers (10 containers) from the first production batch of the tentatively qualified oil procured for U.S. government use (original qualification, reblend, or rebrand) shall be stored at a temperature of not lower than -3 C (-5 F) and not greater than 60 C (140 F) for 1 months (see 4.3.1). At the end of the 1 month storage period, the samples shall be tested in accordance with the conformance tests specified in table IV and Tentative qualification approval. Tentative qualification approval is given to products meeting the qualification inspection (see 4.). Final qualification approval shall be awarded upon successful completion of the stability testing of first production run Failure to pass this test shall be cause for withdrawal of approval Sediment. Sediment measurement may be made using a silver membrane filter. If the total sediment does not exceed 1 mg/l, the ash content does not need to be determined Shear stability. Use an irradiation period of 30 minutes on a 30 ml oil sample at a power setting which causes 11.5 ±0.5 percent viscosity loss to a 30 ml sample of ASTM Reference Fluid, when irradiated for five minutes. ASTM Reference Fluid A is a petroleum oil containing a polymer capable of being broken down by turbulence at high rates of shear; typical viscosities are 10.7 mm /s at 100 C and 57 mm /s at 40 C. ASTM Reference Fluid A may be obtained from vendors listed in the ASTM D603 method. 14

15 4.4.9 Trace metal content. The trace metal content of the oil for qualification testing shall be determined both with a Rotating Disc Electrode - Atomic Emission Spectrometer (RDE-AES) and an Inductively Coupled Plasma - Atomic Emission Spectrometer (ICP-AES) Spectrometer standardization. The spectrometer shall be standardized and correlated in accordance with the JOAP Program Manual, NAVAIR using MIL-DTL standards. Immediately after standardizing the spectrometer, five determinations of the oil for trace metal content shall be performed. The average of the five determinations shall be reported. Samples requiring trace metal content determinations may be sent to: Naval Air Station, Hazmart Building 385, Sample (AIR 4.4.6) NOAP, 680 Hammond Road, Patuxent River, MD ICP adjustments. In accordance with ASTM D5185, modifications that allow for the adjustments in the dilution of the sample are allowed to accurately measure ppm (mg/kg) of metals in the ICP-AES spectrometer Trace metal conformance testing option. Trace metal content for conformance testing (table III) can be tested using either RDE-AES spectrometer or ICP-AES spectrometer for the same elements outlined in table I Corrosion and oxidation stability. The corrosion and oxidation stability test shall be performed in accordance with ASTM D4636, Alternate Procedure, with the following modifications: a. Duplicate tests shall be run at three separate test temperatures, each conducted for a 7-hour duration, at the bath or block temperatures of: 150 ±.5 C (30 ±5 F), 175 ±.5 C (347 ±5 F), and 04 ±.5 C (400 ±5 F). The individual results shall be reported. b. A suitable liquid medium or fluidized sand bath heating apparatus may be used in lieu of an aluminum block heater. c. After the sample tube has been in a liquid heating medium (or aluminum block) for 15 minutes, connect the dry air supply, adjust the air flow rate, and begin the test time. d. An electrolytic grade silver test square shall be substituted for the cadmium plated steel square; stainless steel or nickel-chrome wire may be used to tie the metal coupons together at all test conditions. e. Post-test oil viscosity sample is compared with viscosity of new oil samples tested at 40 C (104 F). Post-test oil total acid number is compared to the total acid number of the new oil sample. The total acid number shall be determined in accordance with SAE ARP5088. f. The glassware from FED-STD-791, method 5308 can be used. The post-test sludge content shall be determined as follows: 15

16 g. Decant oil from the test tube through a preweighed l0.0 micron polytetrafluoroethylene filter (Militec LCWP or equivalent as approved by the qualifying activity) and measure filtrate volume. h. Set filtrate aside for viscosity and acid number tests. i. Remove all sludge from test equipment with rubber policeman, wash equipment and filtered sludge with petroleum ether, oven dry sludge sample, and weigh and compute sludge weight per 100 ml of oil. j. Do not add the petroleum ether washings to the oil filtrate used for viscosity and acid number. Petroleum ether, with a boiling range of 30 to 60 C, n-heptane, or hexane shall be used in place of 1,1,1-trichloroethane (O-T-60) Gear load carrying ability. The average of six determinations shall be not less than 190 percent of the reference oil (Hercolube A, see ), when tested in accordance with FED-STD-791, method 6508 and table II, with the exception that all determinations be performed at an elevated test oil temperature of 100 ±1 C (1 ± F). All six determinations shall be made on the same machine. The reference oil average rating used to obtain the relative ratings shall also be reported. Only the Ryder gear machines having a reference oil average rating of 1,700-,00 lb/in. after eight determinations are acceptable Source for standard reference oil for Ryder Gear Test (see table II). Standard reference oil may be obtained from the Naval Air Systems Command, Attn: AIR 4.4.., Propulsion Lubricants Team, 9 Elmer Road, Building 360, Unit 4, Patuxent River, MD Bearing corrosion. The candidate oil shall successfully pass two series of bearing corrosion tests: a. The first series of tests shall be conducted on the candidate oil as received (new oil) with a minimum of 18 of 36 bearing raceways being free from corrosion; b. The second series shall be conducted on the post-test filtrate from the 150 C corrosion and oxidation stability test (stressed oil) (see table I) with a minimum of 18 of 36 bearing raceways being free from corrosion. c. Any batch of bearing corrosion tests shall also include one pass and one fail reference oil test bearing for quality control purposes. Reference oils shall consist of selected oils qualified under this specification, MIL-PRF-3699, and DOD-PRF Conformance inspection testing methods. The following information is in support of the conformance testing required in table IV Ryder gear load carrying capacity conformance testing. The Ryder Gear test (see table II) shall be performed on the first ten full-scale production lots of each newly qualified lubricating oil supplied to the procuring activity. Additional requirements for performing the Ryder Gear test on subsequent production batches may be specified in the procurement contracts. Additional load carrying test methods may be deemed suitable for qualification of management 16

17 of change issues at the discretion of the qualifying activity. The products shall meet the conformance test requirements as stated in Load carrying conformance test criteria. Lubricating oil products shall exhibit performance greater than or equal to 190 percent of the Hercolube A reference fluid value as measured by six determinations Bearing corrosion conformance inspection procedures. The bearing corrosion test shall be performed on all production batches of the lubricating oil supplied, except as noted in Each production batch of the oil shall successfully pass one series of bearing corrosion tests (see table II) on the new oil. This series shall consist of nine candidate specimens and one each of the pass and fail reference oils (see 4.4.1) Corrosion additive. Confirmation of the presence of the corrosion additive may be conducted using a quantitative laboratory analytical method of analysis approved by the qualifying activity. Confirmation of the specified additive package by such approved methods may be substituted for a bearing corrosion test to satisfy the conformance test requirement. 5. PACKAGING 5.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in the contract or order (see 6.). When packaging of materiel is to be performed by DoD or inhouse contractor personnel, these personnel need to contact the responsible packaging activity to ascertain packaging requirements. Packaging requirements are maintained by the Inventory Control Point's packaging activity within the Military Service or Defense Agency, or within the military service s system commands. Packaging data retrieval is available from the managing Military Department's or Defense Agency's automated packaging files, CD-ROM products, or by contacting the responsible packaging activity. 6. NOTES (This section contains information of a general or explanatory nature that may be helpful, but is not mandatory.) 6.1 Intended use. These lubricating oils are intended for use in helicopter transmission systems. These oils are designed for operation within the approximate bulk oil temperature range of -3 to 00 C (-5 to 39 F). These lubricating oils are also intended for applications where corrosion inhibition is desired. These lubricating oils are not intended for use in gas turbine engine systems. These lubricating oils are not intended for use in gearboxes containing silicone and fluorosilicone seals. 6. Acquisition requirements. Acquisition documents should specify the following: a. Title, number, and date of this specification. b. Quantity required 17

18 c. If certification of conformance to material prohibitions is required (see 3.). d. Submittal of conformance test results (see ). e. Packaging requirements (see 5.1). 6.3 Qualification process. The general outline of the qualification process is described in the SD-6. Clarification information concerning submitting a test sample to the Naval Air System Command for qualification to follows Requesting qualification. At the initiation of the qualification process, prospective suppliers must forward a written request for such action to the Naval Air Systems Command. The activity responsible for qualification is the Naval Air Systems Command, Attn: AIR 4.4.., Propulsion Lubricants Team, 9 Elmer Road, Building 360, Unit 4, Patuxent River, MD Information pertaining to qualification of products may be obtained from that activity. This letter must contain general information on the proposed candidate material. The Naval Air Systems Command will respond in writing with a formal "letter of authorization" providing detailed instructions for the submission of product samples, cost of testing, and test data Qualification sample. Upon receiving authorization by the Naval Air Systems Command, qualification samples may be forwarded to the qualifying activity, as detailed in the authorization letter. These samples will be tested in accordance with the letter of authorization. Each sample must be plainly identified by a securely attached, durable tag or label marked with the following information: QUALIFICATION INSPECTION SAMPLE LUBRICATING OIL, HELICOPTER TRANSMISSION SYSTEM, SYNTHETIC BASE, NATO CODE NUMBER: O-165 Type of sample: (basestock, additive, or finished oil) Name of manufacturer: Product code number: Batch number: Date of manufacture: Submitted by (name) on (date) for qualification inspection in accordance with under authorization of (reference authorizing letter, see 4.) Qualification inspection test report. The manufacturer must submit a certified test report to the qualification activity (see 4.) before any qualification test sample is supplied. Each reformulation request must also include a certified test report. These reports should be submitted in electronic format and use the latest version of the SAE AS5780 Qualified Products Formulation Pro-forma and Qualification Report (see 18

19 Qualification test report requirements. The test report must contain laboratory data performed by the submitter or independent lab showing the results of all tests required by this specification and product classification, with the exception of the tests for compatibility, low temperature storage, stability testing of first production run, gear load carrying ability, and shear stability Formulation Data. The manufacturer must submit the complete formulation data (in hardcopy format) giving the chemical name of each ingredient, the percentage of each ingredient, and the manufacturer and tradename of each ingredient. The manufacturer must use the latest version of the SAE AS5780 Qualified Products Formulation Pro-forma and Qualification Report (see The manufacturer must also submit the MSDS of the candidate product and for each of the additive components used in the formulation. 6.4 Qualification. With respect to products requiring qualification, awards will be made only for the products which are, at the time of award of contract, qualified for inclusion in the Qualified Products List, QPL-3538, whether or not such products have actually been so listed by that date. The attention of the contractors is called to these requirements, and manufacturers are urged to arrange to have the products that they propose to offer to the Federal Government tested for qualification in order that they may be eligible to be awarded contracts or orders for the products covered by this specification. Information pertaining to qualification of products may be obtained from the Naval Air Systems Command, Attn: AIR 4.4.., Propulsion Lubricants Team, 9 Elmer Road, Building 360, Unit 4, Patuxent River, MD Qualified Products Database. Current oils qualified to this specification can be found at Manufacturers with oils qualified to this specification are required to update their CAGE code listing annually at Even if an oil formulation does not have any changes (as described in 4.), manufacturers are required to recertify their products every two years. 6.6 Subject term (key word) listing. Corrosion inhibition Lubricant 6.7 International standardization agreement implementation. This specification implements NATO STANAG1135. When amendment, revision, or cancellation of this specification is proposed, the preparing activity must coordinate the action with the U.S. National Point of Contact for the international standardization agreement, as identified in the ASSIST database at Toxicity. Questions pertinent to this effect should be referred by the contracting activity to the appropriate departmental medical service who will act as its advisor. 19

20 6.8.1 Safety Data Sheets (SDSs). Contracting officers will identify those activities requiring copies of completed Safety Data Sheets prepared in accordance with FED-STD-313. The pertinent Government mailing addresses for submission of data are listed in FED-STD Definitions. Bulk lot - A bulk lot is defined as an indefinite quantity of homogeneous mixture of material offered for acceptance in a single isolated container or manufactured by a single plant run (not exceeding 4 hours) through the same processing equipment, with no change in ingredient material. Packaged lot - A packaged lot is defined as an indefinite number of 08 liter (55 gallon) drums or smaller unit packages of identical size and type offered for acceptance and filled with a homogeneous mixture of material manufactured by a single plant run (not exceeding 4 hours) through the same processing equipment, with no change in ingredient material. 0

21 APPPENDIX A METHOD FOR DETERMINING CORROSION PREVENTATIVE PROPERTIES OF SYNTHETIC GAS TURBINE LUBRICANTS A.1 SCOPE A.1.1 This test method uses ASTM D1743 as a basis to determine the corrosion preventative properties of synthetic gas turbine lubricants using tapered roller bearings stored under wet conditions. This Appendix is a mandatory part of the specification. The information contained herein is intended for compliance. A. APPLICABLE DOCUMENTS ASTM INTERNATIONAL ASTM D1141 ASTM D1193 ASTM D1743 ASTM D35 Standard Practice for the Preparation of Substitute Ocean Water Standard Specification for Reagent Water Standard Test Method for Determining Corrosion Preventative Properties Mineral Spirits (Petroleum Spirits) (Hydrocarbon Dry Cleaning Solvent) (Copies of these documents are available from A.3 TERMINOLOGY A.3.1 Description of terms specific to this specification. Corrosion - the chemical or electrochemical reaction between a material, usually a metal, and its environment that produces a deterioration of the material and its properties. A.4 SUMMARY OF TEST METHOD A.4.1 Summary. Clean, new bearings are immersed in an aviation gas turbine lubricant and rotated, so as to evenly distribute the lubricant over the bearing surfaces. The bearings are subsequently dipped in distilled water, then stored at 5º ± 1 ºC and 100 percent relative humidity. After a specified time period, the bearings are cleaned and the races of the bearing cups are examined for evidence of corrosion. A.5 SIGNIFICANCE AND USE A.5.1 Significance and use. This test method differentiates the relative corrosion preventative capabilities of aviation gas turbine lubricants under the conditions of the test. A.6 APPARATUS a. Timken bearings: Each bearing consists of separate parts. b. Bearing Cone: consisting of cone and roller assembly (Timken Part No. LM 11949). c. Bearing Cup (Timken Part No. LM 11910). 1

22 APPPENDIX A d. Container, 37 cm 3 clear glass jar (85.7 mm high, 69.8 mm diameter) fitted with a lid containing a PTFE 1 liner. Note the lids shall be replaced after 10 tests or earlier if it is apparent that the jar has not remained sealed throughout the test (refer to A.10a and A.10b). e. Bearing Support, a glass adapter with a taper between the range of 14/35 to 19/38 is suitable. f. Glass rod fitted with a rubber policeman. g. Watch glass or alternative glassware that can withstand heating to 71 ºC in an oven (the size required will depend on the number of bearings being prepared). h. Oven, air-circulating, capable of maintaining the temperatures 5º ±1ºC and 71º ±1ºC. (Note the oven should be dark inside and in an area essentially free of vibration.) A.7 REAGENTS a. Distilled Water (ASTM D1193 Type II reagent grade). b. Isopropyl alcohol (Reagent grade) c. Solvent rinse solution: Isopropyl alcohol 90% Distilled Water 9% Ammonium Hydroxide 3 1% (Reagent Grade) d. Stoddard Solvent 4 (as described in specification ASTM D35). e. Synthetic seawater (as described in specification ASTM D1141, combined stock solution 1 and ). f. 50:50 mixture by volume of Isopropyl alcohol and Stoddard solvent A.8 PREPARATION OF BEARINGS A.8.1 Bearing examination. Examine the test bearings carefully and only select those that are entirely free of corrosion. During the bearing preparation handle the bearing with tongs. Care shall be taken to avoid touching the bearings with fingers. A.8. Bearing cleaning procedure. The procedure below describes the use of heated solvents to clean the bearings. The solvents shall only be heated under a suitable fume extraction system. 1 Polytetrafluoroethylene Warning: Flammable 3 Warning: Poison. Causes burns. Vapor extremely irritating. Can be fatal if swallowed. Harmful if inhaled. 4 Warning: Combustible, Vapor Harmful.

23 APPPENDIX A a. Separate and wash the selected bearing thoroughly in hot (5º to 66 ºC) Stoddard solvent to remove rust preventative. To ensure complete removal of the rust preventative, subject the bearing to a second wash in Stoddard solvent heated to between 5º and 66 ºC. b. Remove the bearing from the Stoddard solvent and immerse in solvent rinse solution at ambient temperature. This is to remove the Stoddard solvent and any fingerprints that are present. c. Transfer the bearing from the ambient solvent rinse solution to fresh solvent rinse solution heated to between 66 ºC and 100 ºC. d. Assemble the cup and cone on a bearing support (A.6e) and slowly rotate the bearing while immersed using the glass fitted with a rubber policeman. e. Remove the bearing from the solvent rinse solution, separate the two components and place on a filter paper to drain. f. Transfer the bearing to a watch glass (or alternative glassware) and place this in an oven set at 71º ±1 ºC for 15 minutes to dry the bearing. g. Remove the bearing from the oven and place it in a dessicator to cool for a minimum of 30 minutes. h. When cooled re-examine the bearing to ensure the surfaces are still free of corrosion and the bearing can be turned freely. (Care should be taken not to spin the bearings once they have been prepared as this may damage the race.) A.9 PROCEDURE a. For each test, select bearings that are entirely free of corrosion. The bearings shall only be handled while wearing clean, oil resistant gloves. b. Separate the bearing cup and cone and immerse both components in the test oil. Leave to stand for 10 minutes at ambient temperature. c. Assemble the bearing cup and cone and place it on the glass support in such a manner that the weight of the cup will maintain contact between the races and rolling elements. d. Hold the glass support and re-immerse the bearing in the test oil at ambient temperature, and slowly rotate the cup for 30 seconds using the glass rod fitted with a rubber policeman. Remove the glass support and bearing from the test oil and allow to drain for one minute. e. After draining, completely immerse the glass support and bearing for 10 seconds in freshly boiled distilled water that has been allowed to cool to room temperature. Use a new supply of water for each bearing. f. Add 5 ml of synthetic seawater to a glass jar (see A.6d). Transfer the bearing and glass support from the distilled water to the glass jar, allowing any water on the bearing to remain. Tighten the screw cap firmly and store the jar in a dark oven, located in an area essentially free of vibration, at 5º ±1 ºC for 48 hours. 3

24 APPPENDIX A A.10 RATING PROCEDURE a. Upon completion of the storage period, remove the jars from the oven. Visually determine if any condensation is present in the sealed jars. If condensation is not present, then the PTFE liner of the lid should be considered suspect and the lid should be replaced. b. Remove the bearing from the test jar. An audible hiss is often heard when the lid seal is broken, which adds further confidence in the sealing ability of the lid. c. Remove the bearing from the jar and separate the two components. Place the bearing cup in a 50:50 mixture by volume of isopropyl alcohol and Stoddard solvent. The solvent mixture can be heated to facilitate the removal of the oil, while observing the proper precautions for a flammable mixture. Agitate the cup vigorously to remove the oil. d. Transfer the bearing cup from the solvent and allow to dry on clean filter paper. e. Wipe the cup raceway with lint free paper, so as to remove any staining and repeat the rinsing using fresh solvent mixture if necessary to ensure all traces of the oil and stains are removed. f. Examine the cup raceway for evidence of corrosion without the use of magnification using the IP 0 rating criteria as shown in table A-I. Record the rating for each bearing. TABLE A-I. Rating criteria. Rating Degree of Corrosion 0 No corrosion No more than three small spots sufficient to be visible to the naked eye and less than 1 mm in diameter. Small areas of corrosion covering up to 1% of the surface. Areas of corrosion covering between 1% and 5% of the surface. Areas of corrosion covering between 5% and 10% of the surface. Areas of corrosion covering more than 10% of the surface A.11 REPORT A.11.1 Test result report. Report the test result as the total count of bearings tested in the test oil, the number of bearings that were recorded for each rating category, and the recorded rating of the pass and fail reference oil. 4

25 CONCLUDING MATERIAL Custodians: Preparing activity: Army - AT Navy - AS Navy - AS (Project ) Air Force - 0 DLA - GS Review activities: Army - AV Navy - SH Air Force - 68 NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at 5

PERFORMANCE SPECIFICATION LUBRICATING OIL, JET ENGINE

PERFORMANCE SPECIFICATION LUBRICATING OIL, JET ENGINE INCH-POUND 12 December 2014 SUPERSEDING MIL-PRF-6081D w/amendment 1 30 January 2009 PERFORMANCE SPECIFICATION LUBRICATING OIL, JET ENGINE This specification is approved for use by all Departments and Agencies

More information

PERFORMANCE SPECIFICATION LUBRICATING OIL, HELICOPTER TRANSMISSION SYSTEM, SYNTHETIC BASE

PERFORMANCE SPECIFICATION LUBRICATING OIL, HELICOPTER TRANSMISSION SYSTEM, SYNTHETIC BASE METRIC 9 June 004 SUPERSEDING DOD-L-85734 (AS) 1 February 1986 PERFORMANCE SPECIFICATION LUBRICATING OIL, HELICOPTER TRANSMISSION SYSTEM, SYNTHETIC BASE This specification is approved for use by all Departments

More information

PERFORMANCE SPECIFICATION. LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE, NATO CODE NUMBERS: O-152, O-154, O-156, and O-167

PERFORMANCE SPECIFICATION. LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE, NATO CODE NUMBERS: O-152, O-154, O-156, and O-167 METRIC 13 March 014 SUPERSEDING MIL-PRF-3699F 1 May 1997 PERFORMANCE SPECIFICATION LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE, NATO CODE NUMBERS: O-15, O-154, O-156, and O-167 This specification

More information

MILITARY SPECIFICATION LUBRICATING OIL, VACUUM PUMP, MECHANICAL

MILITARY SPECIFICATION LUBRICATING OIL, VACUUM PUMP, MECHANICAL INCH-POUND MIL-DTL-83767C 24 September 2007 SUPERSEDING MIL-L-83767B 8 February 1980 MILITARY SPECIFICATION LUBRICATING OIL, VACUUM PUMP, MECHANICAL Reactivated after 24 September 2007 and may be used

More information

PERFORMANCE SPECIFICATION

PERFORMANCE SPECIFICATION METRIC 05 November 2015 SUPERSEDING MIL-PRF-7870D 30 April 2010 PERFORMANCE SPECIFICATION LUBRICATING OIL: GENERAL PURPOSE, LOW-TEMPERATURE (NATO O-142) This specification is approved for use by all Departments

More information

PERFORMANCE SPECIFICATION LUBRICATING OIL, JET ENGINE

PERFORMANCE SPECIFICATION LUBRICATING OIL, JET ENGINE INCH-POUND 10 November 1997 SUPERSEDING MIL-L-6081C 15 April 1964 PERFORMANCE SPECIFICATION LUBRICATING OIL, JET ENGINE This specification is approved for use by all Departments and Agencies of the Department

More information

PERFORMANCE SPECIFICATION GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE, NATO CODE G-395

PERFORMANCE SPECIFICATION GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE, NATO CODE G-395 METRIC 24 January 2005 SUPERSEDING MIL-PRF-81322F 21 July 1998 PERFORMANCE SPECIFICATION GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE, NATO CODE G-395 This specification is approved for use

More information

PERFORMANCE SPECIFICATION CALIBRATING FLUIDS, AIRCRAFT FUEL SYSTEM COMPONENTS

PERFORMANCE SPECIFICATION CALIBRATING FLUIDS, AIRCRAFT FUEL SYSTEM COMPONENTS METRIC 20 January 2012 SUPERSEDING MIL-PRF-7024E 1 October 1997 PERFORMANCE SPECIFICATION CALIBRATING FLUIDS, AIRCRAFT FUEL SYSTEM COMPONENTS Comments, suggestions, or questions on this document should

More information

PERFORMANCE SPECIFICATION COOLANT FLUID, HYDROLYTICALLY STABLE, DIELECTRIC

PERFORMANCE SPECIFICATION COOLANT FLUID, HYDROLYTICALLY STABLE, DIELECTRIC INCH-POUND w/amendment 1 29 December 2004 SUPERSEDING 24 October 1997 PERFORMANCE SPECIFICATION COOLANT FLUID, HYDROLYTICALLY STABLE, DIELECTRIC This specification is approved for use by all Departments

More information

FEDERAL SPECIFICATION ETHER, PETROLEUM; TECHNICAL GRADE. 1.1 Scope. This specification covers technical grade petroleum ether to be used as a solvent.

FEDERAL SPECIFICATION ETHER, PETROLEUM; TECHNICAL GRADE. 1.1 Scope. This specification covers technical grade petroleum ether to be used as a solvent. METRIC 4 May 2015 SUPERSEDING O-E-751C 10 January 2003 FEDERAL SPECIFICATION ETHER, PETROLEUM; TECHNICAL GRADE The General Services Administration has authorized the use of this federal specification by

More information

PERFORMANCE SPECIFICATION CORROSION-PREVENTIVE, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE

PERFORMANCE SPECIFICATION CORROSION-PREVENTIVE, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE INCH-POUND MIL-PRF-8188D 10 December 1997 SUPERSEDING MIL-C-8188C 26 May 1959 PERFORMANCE SPECIFICATION CORROSION-PREVENTIVE, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE This specification is approved for

More information

PERFORMANCE SPECIFICATION HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537

PERFORMANCE SPECIFICATION HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 METRIC MIL-PRF-83282D 30 September 1997 SUPERSEDING MIL-H-83282C 25 March 1986 MIL-H-83282C Interim Amendment 1 31 January 1997 PERFORMANCE SPECIFICATION HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON

More information

UNIFIED FACILITIES GUIDE SPECIFICATIONS

UNIFIED FACILITIES GUIDE SPECIFICATIONS USACE / NAVFAC / AFCEC / NASA UFGS-48 06 15 (May 2014) ---------------------------------- Preparing Activity: USACE Superseding UFGS-48 13 19.00 10 (January 2008) UNIFIED FACILITIES GUIDE SPECIFICATIONS

More information

MILITARY SPECIFICATION LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE

MILITARY SPECIFICATION LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE INCH POUND 20 July 1994 SUPERSEDING MIL L 7808J 11 May 1982 MILITARY SPECIFICATION LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE This specification is approved for use by all Departments and

More information

FEDERAL SPECIFICATION METHANOL (METHYL ALCOHOL) 1.1 Scope. This specification covers three grades and four unit quantities of methanol.

FEDERAL SPECIFICATION METHANOL (METHYL ALCOHOL) 1.1 Scope. This specification covers three grades and four unit quantities of methanol. NOT MEASUREMENT SENSITIVE 19 January 2016 SUPERSEDING O-M-232L 4 January 2006 FEDERAL SPECIFICATION METHANOL (METHYL ALCOHOL) The General Services Administration has authorized the use of this federal

More information

PERFORMANCE SPECIFICATION COOLANT FLUID, HYDROLYTICALLY STABLE, DIELECTRIC

PERFORMANCE SPECIFICATION COOLANT FLUID, HYDROLYTICALLY STABLE, DIELECTRIC INCH-POUND 24 October 1997 SUPERSEDING MIL-C-87252B 25 August 1993 PERFORMANCE SPECIFICATION COOLANT FLUID, HYDROLYTICALLY STABLE, DIELECTRIC This specification is approved for use by all Departments and

More information

PERFORMANCE SPECIFICATION HYDRAULIC FLUID, PETROLEUM, INHIBITED

PERFORMANCE SPECIFICATION HYDRAULIC FLUID, PETROLEUM, INHIBITED METRIC MIL-PRF-17672E 14 October 2010 SUPERSEDING MIL-PRF-17672D 23 January 1984 PERFORMANCE SPECIFICATION HYDRAULIC FLUID, PETROLEUM, INHIBITED This specification is approved for use by all Departments

More information

PERFORMANCE SPECIFICATION GREASE, AIRCRAFT AND INSTRUMENT, FUEL AND OXIDIZER RESISTANT

PERFORMANCE SPECIFICATION GREASE, AIRCRAFT AND INSTRUMENT, FUEL AND OXIDIZER RESISTANT METRIC 15 August 211 SUPERSEDING MILPRF27617F 17 February 1998 PERFORMANCE SPECIFICATION GREASE, AIRCRAFT AND INSTRUMENT, FUEL AND OXIDIZER RESISTANT Comments, suggestions, or questions on this document

More information

PERFORMANCE SPECIFICATION GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE

PERFORMANCE SPECIFICATION GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE METRIC 21 July 1998 SUPERSEDING MIL-G-81322E 22 January 1992 PERFORMANCE SPECIFICATION GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE This specification is approved for use by all Departments

More information

MILITARY SPECIFICATION CORROSION PREVENTIVE COMPOUNDS, WATER DISPLACING, ULTRA-THIN FILM PAGE 1

MILITARY SPECIFICATION CORROSION PREVENTIVE COMPOUNDS, WATER DISPLACING, ULTRA-THIN FILM PAGE 1 NOT MEASUREMENT SENSITIVE 26 November 1997 SUPERSEDING AMENDMENT 2 31 July 1996 MILITARY SPECIFICATION CORROSION PREVENTIVE COMPOUNDS, WATER DISPLACING, ULTRA-THIN FILM This amendment forms a part of,

More information

DETAIL SPECIFICATION HYDRAULIC & LUBRICATING OIL, SYNTHETIC HYDROCARBON BASE

DETAIL SPECIFICATION HYDRAULIC & LUBRICATING OIL, SYNTHETIC HYDROCARBON BASE METRIC 24 August 2012 SUPERSEDING MIL-DTL-32353 1 June 2010 1. SCOPE DETAIL SPECIFICATION HYDRAULIC & LUBRICATING OIL, SYNTHETIC HYDROCARBON BASE This specification is approved for use by all Departments

More information

COMMERCIAL ITEM DESCRIPTION DRY CLEANING AND DEGREASING SOLVENT, PD680

COMMERCIAL ITEM DESCRIPTION DRY CLEANING AND DEGREASING SOLVENT, PD680 NOT MEASUREMENT SENSITIVE 27 September 00 COMMERCIAL ITEM DESCRIPTION DRY CLEANING AND DEGREASING SOLVENT, PD680 The General Services Administration has authorized the use of this commercial item description

More information

Joint Oil Analysis Program Spectrometer Standards SCP Science (Conostan) Qualification Report For D19-0, D3-100, and D12-XXX Series Standards

Joint Oil Analysis Program Spectrometer Standards SCP Science (Conostan) Qualification Report For D19-0, D3-100, and D12-XXX Series Standards Joint Oil Analysis Program Spectrometer Standards SCP Science (Conostan) Qualification Report For D19-0, D3-100, and D12-XXX Series Standards NF&LCFT REPORT 441/15-008 Prepared By: MICHAEL PERETICH, PHD

More information

PERFORMANCE SPECIFICATION COOLERS, LUBRICATING OIL, AIRCRAFT, GENERAL SPECIFICATION FOR

PERFORMANCE SPECIFICATION COOLERS, LUBRICATING OIL, AIRCRAFT, GENERAL SPECIFICATION FOR INCH-POUND 06 May 2013 SUPERSEDING MIL-PRF-25478C 29 December 1997 PERFORMANCE SPECIFICATION COOLERS, LUBRICATING OIL, AIRCRAFT, GENERAL SPECIFICATION FOR This specification is approved for use by all

More information

FEDERAL SPECIFICATION CUTTING FLUIDS: EMULSIFIABLE OILS

FEDERAL SPECIFICATION CUTTING FLUIDS: EMULSIFIABLE OILS NOT MEASUREMENT SENSITIVE 19 August 2005 SUPERSEDING VV-V-846B 16 October 1998 FEDERAL SPECIFICATION CUTTING FLUIDS: EMULSIFIABLE OILS The General Services Administration has authorized the use of this

More information

PERFORMANCE SPECIFICATION GREASE, AUTOMOTIVE AND ARTILLERY

PERFORMANCE SPECIFICATION GREASE, AUTOMOTIVE AND ARTILLERY NOT MEASUREMENT SENSITIVE w/ 26 September 2012 SUPERSEDING 30 September 2008 PERFORMANCE SPECIFICATION GREASE, AUTOMOTIVE AND ARTILLERY This specification is approved for use by all Departments and Agencies

More information

Joint Oil Analysis Program Spectrometer Standards VHG Labs Inc. Qualification Report For D19-0, D3-100 and D12-XXX Series Standards

Joint Oil Analysis Program Spectrometer Standards VHG Labs Inc. Qualification Report For D19-0, D3-100 and D12-XXX Series Standards Joint Oil Analysis Program Spectrometer Standards VHG Labs Inc. Qualification Report For D19-0, D3-100 and D12-XXX Series Standards NF&LCFT REPORT 441/13-010 Prepared By: MICHAEL PERETICH, PhD Oil Analysis

More information

DETAIL SPECIFICATION DETECTOR PAD, FREE WATER. This specification is approved for use by all Departments and Agencies of the Department of Defense.

DETAIL SPECIFICATION DETECTOR PAD, FREE WATER. This specification is approved for use by all Departments and Agencies of the Department of Defense. METRIC DETAIL SPECIFICATION DETECTOR PAD, FREE WATER 31 March 2006 SUPERSEDING MIL-D-81248B 30 June 1980 This specification is approved for use by all Departments and Agencies of the Department of Defense.

More information

PERFORMANCE SPECIFICATION LUBRICATING OIL, INSTRUMENT, AIRCRAFT, LOW VOLATILITY

PERFORMANCE SPECIFICATION LUBRICATING OIL, INSTRUMENT, AIRCRAFT, LOW VOLATILITY METRIC 8 December 2011 SUPERSEDING MIL-PRF-6085D 20 February 1998 PERFORMANCE SPECIFICATION LUBRICATING OIL, INSTRUMENT, AIRCRAFT, LOW VOLATILITY Comments, suggestions, or questions on this document should

More information

DETAIL SPECIFICATION FUEL, NAVAL DISTILLATE. This specification is approved for use by all Departments and Agencies of the Department of Defense.

DETAIL SPECIFICATION FUEL, NAVAL DISTILLATE. This specification is approved for use by all Departments and Agencies of the Department of Defense. METRIC 14 August 2012 SUPERSEDING MIL-DTL-16884L 23 October 2006 DETAIL SPECIFICATION FUEL, NAVAL DISTILLATE This specification is approved for use by all Departments and Agencies of the Department of

More information

PERFORMANCE SPECIFICATION HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE

PERFORMANCE SPECIFICATION HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE INCH-POUND MIL-PRF-5606H w/amendment 3 7 September 2006 SUPERSEDING MIL-PRF-5606H w/amendment 2 27 October 2005 PERFORMANCE SPECIFICATION HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE

More information

ÚÄÄÄÄÄÄÄÄÄÄ ÚÄÄÄÄÄÄÄÄÄÄ ³ METRIC ³ ÀÄÄÄÄÄÄÄÄÄÄÙ TT-T-306E May 28, 1993 SUPERSEDING TT-T-306D December 31, 1992 FEDERAL SPECIFICATION

ÚÄÄÄÄÄÄÄÄÄÄ ÚÄÄÄÄÄÄÄÄÄÄ ³ METRIC ³ ÀÄÄÄÄÄÄÄÄÄÄÙ TT-T-306E May 28, 1993 SUPERSEDING TT-T-306D December 31, 1992 FEDERAL SPECIFICATION ÚÄÄÄÄÄÄÄÄÄÄ ÚÄÄÄÄÄÄÄÄÄÄ ³ METRIC ³ ÀÄÄÄÄÄÄÄÄÄÄÙ May 28, 1993 SUPERSEDING TT-T-306D December 31, 1992 FEDERAL SPECIFICATION THINNER, SYNTHETIC RESIN ENAMELS This specification has been approved by the Commissioner,

More information

ENGINEERING AND CONSTRUCTION BULLETIN

ENGINEERING AND CONSTRUCTION BULLETIN ENGINEERING AND CONSTRUCTION BULLETIN No. 2007-21 Issuing Office: CECW-CE Issued: 16 Nov 2007 Subject: Revision to EM 1110-2-1424 Lubricants and Hydraulic Fluids - Appendix C Applicability: Guidance 1.

More information

PERFORMANCE SPECIFICATION LUBRICATING OIL, SHIPBOARD INTERNAL COMBUSTION ENGINE, HIGH-OUTPUT DIESEL

PERFORMANCE SPECIFICATION LUBRICATING OIL, SHIPBOARD INTERNAL COMBUSTION ENGINE, HIGH-OUTPUT DIESEL METRIC MIL-PRF-9000J(SH) 07 January 2010 SUPERSEDING MIL-PRF-9000H(SH) 16 September 1987 PERFORMANCE SPECIFICATION LUBRICATING OIL, SHIPBOARD INTERNAL COMBUSTION ENGINE, HIGH-OUTPUT DIESEL This specification

More information

PERFORMANCE SPECIFICATION LUBRICATING OIL, GENERAL PURPOSE, PRESERVATIVE (WATER-DISPLACING, LOW TEMPERATURE)

PERFORMANCE SPECIFICATION LUBRICATING OIL, GENERAL PURPOSE, PRESERVATIVE (WATER-DISPLACING, LOW TEMPERATURE) NOT MEASUREMENT SENSITIVE MIL-PRF-32033A W/Amendment 1 07 July 2016 MIL-PRF-32033A 16 February 2016 PERFORMANCE SPECIFICATION LUBRICATING OIL, GENERAL PURPOSE, PRESERVATIVE (WATER-DISPLACING, LOW TEMPERATURE)

More information

NOT MEASUREMENT SENSITIVE MIL-PRF-3150E 7 August 2008 SUPERSEDING MIL-PRF-3150D 6 February 1997 PERFORMANCE SPECIFICATION

NOT MEASUREMENT SENSITIVE MIL-PRF-3150E 7 August 2008 SUPERSEDING MIL-PRF-3150D 6 February 1997 PERFORMANCE SPECIFICATION NOT MEASUREMENT SENSITIVE MIL-PRF-3150E 7 August 2008 SUPERSEDING MIL-PRF-3150D 6 February 1997 PERFORMANCE SPECIFICATION LUBRICATING OIL, PRESERVATIVE, MEDIUM This specification is approved for use by

More information

PERFORMANCE SPECIFICATION HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION

PERFORMANCE SPECIFICATION HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION METRIC 26 April 2013 SUPERSEDING MIL-PRF-6083F 17 September 1997 PERFORMANCE SPECIFICATION HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION This specification is approved for use by all

More information

PERFORMANCE SPECIFICATION COOLERS, LUBRICATING OIL, AIRCRAFT, GENERAL SPECIFICATION FOR

PERFORMANCE SPECIFICATION COOLERS, LUBRICATING OIL, AIRCRAFT, GENERAL SPECIFICATION FOR I INCH-POUND 29 December 1997 SUPERSEDING MIL-C-25478B(USAF) 28 March 1995 PERFORMANCE SPECIFICATION COOLERS, LUBRICATING OIL, AIRCRAFT, GENERAL SPECIFICATION FOR This specification is approved for use

More information

INCH-POUND MIL-DTL-24211D 25 February 2016 SUPERSEDING MIL-DTL-24211C 9 February 2011 DETAIL SPECIFICATION

INCH-POUND MIL-DTL-24211D 25 February 2016 SUPERSEDING MIL-DTL-24211C 9 February 2011 DETAIL SPECIFICATION DETAIL SPECIFICATION INCH-POUND MIL-DTL-24211D 25 February 2016 SUPERSEDING MIL-DTL-24211C 9 February 2011 GASKETS, WAVEGUIDE FLANGE GENERAL SPECIFICATION FOR 1. SCOPE This specification is approved for

More information

DETAIL SPECIFICATION RUBBER, FLUOROSILICONE ELASTOMER, OIL AND FUEL RESISTANT, SHEETS, STRIPS, MOLDED PARTS, AND EXTRUDED SHAPES

DETAIL SPECIFICATION RUBBER, FLUOROSILICONE ELASTOMER, OIL AND FUEL RESISTANT, SHEETS, STRIPS, MOLDED PARTS, AND EXTRUDED SHAPES INCH-POUND 11 August 2006 SUPERSEDING MIL-R-25988B 12 July 1983 DETAIL SPECIFICATION RUBBER, FLUOROSILICONE ELASTOMER, OIL AND FUEL RESISTANT, SHEETS, STRIPS, MOLDED PARTS, AND EXTRUDED SHAPES Reactivated

More information

DETAIL SPECIFICATION SHEET

DETAIL SPECIFICATION SHEET METRIC MIL-DTL-38999/31E 12 March 2014 SUPERSEDING MIL-DTL-38999/31D 19 April 2002 DETAIL SPECIFICATION SHEET CONNECTORS, ELECTRICAL, CIRCULAR, THREADED, PLUG, LANYARD RELEASE, FAIL-SAFE, REMOVABLE CRIMP

More information

DETAIL SPECIFICATION SHEET DISK, VALVE. Inactive for new design after 15 October 1998.

DETAIL SPECIFICATION SHEET DISK, VALVE. Inactive for new design after 15 October 1998. INCH-POUND MS29521H 23 September 2015 SUPERSEDING MS29521G 7 April 2009 DETAIL SPECIFICATION SHEET DISK, VALVE Inactive for new design after 15 October 1998. This specification is approved for use by all

More information

VHG Labs, Inc. Standards and Supplies for Spectrochemical Oil Analysis

VHG Labs, Inc. Standards and Supplies for Spectrochemical Oil Analysis VHG Labs, Inc. Standards and Supplies for Spectrochemical Oil Analysis Metallo-Organic Standards from VHG Labs VHG Labs has been a provider of quality analytical products and services for over 25 years.

More information

PERFORMANCE SPECIFICATION ACTUATOR, LINEAR, ELECTROMECHANICAL

PERFORMANCE SPECIFICATION ACTUATOR, LINEAR, ELECTROMECHANICAL INCH-POUND PERFORMANCE SPECIFICATION 17 September 2015 SUPERSEDING MIL-A-85046(AS) 7 September 1976 ACTUATOR, LINEAR, ELECTROMECHANICAL This specification is approved for use by the Naval Air Systems Command

More information

DETAIL SPECIFICATION SHEET

DETAIL SPECIFICATION SHEET INCH-POUND MIL-DTL-24308/24H 8 June 2018 SUPERSEDING MIL-DTL-24308/24H w/amendment 4 8 April 2015 DETAIL SPECIFICATION SHEET CONNECTORS, ELECTRIC, RECTANGULAR, NONENVIRONMENTAL, MINIATURE, POLARIZED SHELL,

More information

Paragon Scientific Ltd Proficiency Testing Scheme Schedule

Paragon Scientific Ltd Proficiency Testing Scheme Schedule Paragon Scientific Ltd Proficiency Testing Scheme Schedule Proficiency Testing Scheme Schedule Page 1 of 16 Issue : 29/01/2015 Print : 25/06/2018 Viscosity ASTM D445 - Standard Test Method for Kinematic

More information

DETAIL SPECIFICATION GASKETS, WAVEGUIDE FLANGE GENERAL SPECIFICATION FOR

DETAIL SPECIFICATION GASKETS, WAVEGUIDE FLANGE GENERAL SPECIFICATION FOR INCH-POUND 25 November 1998 SUPERSEDING MIL-G-24211 28 MARCH 1966 DETAIL SPECIFICATION GASKETS, WAVEGUIDE FLANGE GENERAL SPECIFICATION FOR This specification is approved for use by all Departments and

More information

1.1 Unless otherwise stated, the specification references and test methods are from the latest version in effect at the time of this contract.

1.1 Unless otherwise stated, the specification references and test methods are from the latest version in effect at the time of this contract. (Page 1 of 6) LUBRICATING PRODUCTS MGS-92-12K 1.0 DESCRIPTION. This specification covers motor vehicle lubricating products for delivery in prepackaged containers such as drums, pails, etc., or for delivery

More information

COMMERCIAL ITEM DESCRIPTION HOSE AND HOSE ASSEMBLIES, NONMETALLIC SPRAY

COMMERCIAL ITEM DESCRIPTION HOSE AND HOSE ASSEMBLIES, NONMETALLIC SPRAY [INCH-POUND] A-A-59613 August 16, 2001 SUPERSEDING ZZ-H-521F May 28, 1993 COMMERCIAL ITEM DESCRIPTION HOSE AND HOSE ASSEMBLIES, NONMETALLIC SPRAY The General Services Administration has authorized the

More information

PERFORMANCE SPECIFICATION ADDITIVE, LUBRICITY IMPROVER, DIESEL

PERFORMANCE SPECIFICATION ADDITIVE, LUBRICITY IMPROVER, DIESEL METRIC MIL-PRF-32490 03 February 2014 PERFORMANCE SPECIFICATION ADDITIVE, LUBRICITY IMPROVER, DIESEL This specification is approved for use by all Departments and Agencies of the Department of Defense.

More information

PERFORMANCE SPECIFICATION DEGREASING SOLVENT

PERFORMANCE SPECIFICATION DEGREASING SOLVENT NOT MEASUREMENT SENSITIVE 13 December 1999 SUPERSEDING P-D-680B October 29, 1992 PERFORMANCE SPECIFICATION DEGREASING SOLVENT This specification is approved for use by all Departments and Agencies of the

More information

DEPARTMENT OF DEFENSE INTERFACE STANDARD

DEPARTMENT OF DEFENSE INTERFACE STANDARD INCH-POUND MIL-STD-1560C 23 January 2017 SUPERSEDING MIL-STD-1560C 11 February 2015 DEPARTMENT OF DEFENSE INTERFACE STANDARD INSERT ARRANGEMENTS FOR MIL-DTL-38999, MIL-DTL-27599, AND SAE-AS29600 SERIES

More information

Draft Indian Standard SYN GAS/ AMMONIA TURBO COMPRESSOR LUBRICATING OILS SPECIFICATION

Draft Indian Standard SYN GAS/ AMMONIA TURBO COMPRESSOR LUBRICATING OILS SPECIFICATION Comments Only BUREAU OF INDIAN STANDARDS Draft Indian Standard Doc:PCD 3(2537)C September 2012 SYN GAS/ AMMONIA TURBO COMPRESSOR LUBRICATING OILS SPECIFICATION Not to be reproduced without the permission

More information

MATERIAL AND EQUIPMENT STANDARD FOR FAST DRYING SYNTHETIC PRIMER TO BE USED WITH HOT APPLIED COAL TAR OR BITUMEN (ASPHALT) ENAMEL ORIGINAL EDITION

MATERIAL AND EQUIPMENT STANDARD FOR FAST DRYING SYNTHETIC PRIMER TO BE USED WITH HOT APPLIED COAL TAR OR BITUMEN (ASPHALT) ENAMEL ORIGINAL EDITION MATERIAL AND EQUIPMENT STANDARD FOR FAST DRYING SYNTHETIC PRIMER TO BE USED WITH HOT APPLIED COAL TAR OR BITUMEN (ASPHALT) ENAMEL ORIGINAL EDITION OCT. 1996 This standard specification is reviewed and

More information

DETAIL SPECIFICATION TURBINE FUEL, AVIATION, THERMALLY STABLE (JPTS)

DETAIL SPECIFICATION TURBINE FUEL, AVIATION, THERMALLY STABLE (JPTS) METRIC (USAF) 25 July 2016 SUPERSEDING (USAF) 04 September 2015 DETAIL SPECIFICATION TURBINE FUEL, AVIATION, THERMALLY STABLE (JPTS) This specification is approved for use by the Department of the Air

More information

Downloaded from

Downloaded from December 20, 1989 TO SUPERSEDE W-F-408D 30 March 1984 FEDERAL SPECIFICATION FITTINGS FOR CONDUIT, METAL, RIGID (THICK-WALL AND THIN-WALL (EMT) TYPE) This specification is approved by the Commissioner.

More information

COMMERCIAL ITEM DESCRIPTION PINTLE ASSEMBLY, TOWING, MANUAL RELEASE, , AND LBS CAPACITY

COMMERCIAL ITEM DESCRIPTION PINTLE ASSEMBLY, TOWING, MANUAL RELEASE, , AND LBS CAPACITY [INCH-POUND] July 30, 1996 SUPERSEDING (see 7.5) COMMERCIAL ITEM DESCRIPTION PINTLE ASSEMBLY, TOWING, MANUAL RELEASE, 18 000, 40 000 AND 100 000 LBS CAPACITY The General Services Administration has authorized

More information

PERFORMANCE SPECIFICATION LUBRICATING OIL, STEAM TURBINE AND GEAR, MODERATE SERVICE

PERFORMANCE SPECIFICATION LUBRICATING OIL, STEAM TURBINE AND GEAR, MODERATE SERVICE METRIC 09 September 2003 SUPERSEDING MIL-PRF-17331H(SH) 23 January 1984 1. SCOPE PERFORMANCE SPECIFICATION LUBRICATING OIL, STEAM TURBINE AND GEAR, MODERATE SERVICE This specification is approved for use

More information

DETAIL SPECIFICATION TURBINE FUEL, AVIATION, GRADES JP-4 and JP-5

DETAIL SPECIFICATION TURBINE FUEL, AVIATION, GRADES JP-4 and JP-5 METRIC 5 January 2004 SUPERSEDING MIL-DTL-5624T 18 September 1998 DETAIL SPECIFICATION TURBINE FUEL, AVIATION, GRADES JP-4 and JP-5 This specification is approved for use by all Departments and Agencies

More information

DETAIL SPECIFICATION SHEET

DETAIL SPECIFICATION SHEET METRIC MIL-DTL-38999/36 30 November 2006 DETAIL SPECIFICATION SHEET CONNECTORS, ELECTRICAL, CIRCULAR, THREADED, PLUG, LANYARD RELEASE, FAIL-SAFE, REMOVABLE CRIMP CONTACTS, PINS, SHELL SIZE 25, SERIES III,

More information

PERFORMANCE SPECIFICATION CLEANING COMPOUND, SOLVENT (FOR BORE OF WEAPONS)

PERFORMANCE SPECIFICATION CLEANING COMPOUND, SOLVENT (FOR BORE OF WEAPONS) PERFORMANCE SPECIFICATION INCH-POUND 05 November 2013 SUPERSEDING MIL-PRF-372D 10 July 1998 CLEANING COMPOUND, SOLVENT (FOR BORE OF WEAPONS) This specification is approved for use by all Departments and

More information

QQ-W-343F 19 November 1990 (TO SUPERSEDE) QQ-W-343-E November 13, 1981 FEDERAL SPECIFICATION WIRE, ELECTRICAL, COPPER (UNINSULATED)

QQ-W-343F 19 November 1990 (TO SUPERSEDE) QQ-W-343-E November 13, 1981 FEDERAL SPECIFICATION WIRE, ELECTRICAL, COPPER (UNINSULATED) 19 November 1990 (TO SUPERSEDE) QQ-W-343-E November 13, 1981 FEDERAL SPECIFICATION WIRE, ELECTRICAL, COPPER (UNINSULATED) 1. SCOPE AND CLASSIFICATION 1.1 Scope. This specification covers solid, bunch-stranded,

More information

PERFORMANCE SPECIFICATION SHEET BATTERY, STORAGE, AIRCRAFT, MAINTENANCE-FREE, 24-VOLT, 1.5-AMPERE-HOUR

PERFORMANCE SPECIFICATION SHEET BATTERY, STORAGE, AIRCRAFT, MAINTENANCE-FREE, 24-VOLT, 1.5-AMPERE-HOUR METRIC MIL-PRF-8565/6A (AS) 25 June 2001 SUPERSEDING DOD-B-8565/6(AS) 26 June 1987 PERFORMANCE SPECIFICATION SHEET BATTERY, STORAGE, AIRCRAFT, MAINTENANCE-FREE, 24-VOLT, 1.5-AMPERE-HOUR This specification

More information

PERFORMANCE SPECIFICATION HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE

PERFORMANCE SPECIFICATION HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE INCH-POUND MIL-PRF-566H 7 June 22 SUPERSEDING MIL-H-566G 9 September 1994 PERFORMANCE SPECIFICATION HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE Inactive for new design after 29 March

More information

PERFORMANCE SPECIFICATION SHEET SWITCHES, SENSITIVE, PLUNGER, 10 AMPERES 2PDT AND 7 AMPERES 4PDT, RESILIENT SEAL

PERFORMANCE SPECIFICATION SHEET SWITCHES, SENSITIVE, PLUNGER, 10 AMPERES 2PDT AND 7 AMPERES 4PDT, RESILIENT SEAL INCH-POUND MIL-PRF-8805/100G 6 December 2012 SUPERSEDING MIL-PRF-8805/100F 4 October 2004 PERFORMANCE SPECIFICATION SHEET SWITCHES, SENSITIVE, PLUNGER, 10 AMPERES 2PDT AND 7 AMPERES 4PDT, RESILIENT SEAL

More information

QQ-A-250/11F August SUPERSEDING QQ-A-250/GEN. August 27, 1971 FEDERAL SPECIFICATION SHEET ALUMINUM ALLOY 6061, PLATE AND SHEET

QQ-A-250/11F August SUPERSEDING QQ-A-250/GEN. August 27, 1971 FEDERAL SPECIFICATION SHEET ALUMINUM ALLOY 6061, PLATE AND SHEET August 3 1982 SUPERSEDING QQ-A-250/11E August 27, 1971 FEDERAL SPECIFICATION SHEET ALUMINUM ALLOY 6061, PLATE AND SHEET This specification is approved by the Commissioner, Federal Supply Service, General

More information

MILITARY SPECIFICATION MICROCIRCUITS, LINEAR, CMOS, ANALOG SWITCH WITH DRIVER, MONOLITHIC SILICON

MILITARY SPECIFICATION MICROCIRCUITS, LINEAR, CMOS, ANALOG SWITCH WITH DRIVER, MONOLITHIC SILICON INCH-POUND 4 February 2004 SUPERSEDING MIL-M-38510/116 16 April 1980 MILITARY SPECIFICATION MICROCIRCUITS, LINEAR, CMOS, ANALOG SWITCH WITH DRIVER, MONOLITHIC SILICON This specification is approved for

More information

COMMERCIAL ITEM DESCRIPTION BEARING, BALL, ANNULAR, SINGLE ROW, RADIAL, NON-FILLING SLOT, DIMENSION SERIES 02

COMMERCIAL ITEM DESCRIPTION BEARING, BALL, ANNULAR, SINGLE ROW, RADIAL, NON-FILLING SLOT, DIMENSION SERIES 02 METRIC A-A-59584C 15 September 2008 SUPERSEDING A-A-59584B 23 September 2003 COMMERCIAL ITEM DESCRIPTION BEARING, BALL, ANNULAR, SINGLE ROW, RADIAL, NON-FILLING SLOT, DIMENSION SERIES 02 The General Services

More information

DETAIL SPECIFICATION PROPELLANT, HIGH DENSITY SYNTHETIC HYDROCARBON TYPE, GRADE JP-10

DETAIL SPECIFICATION PROPELLANT, HIGH DENSITY SYNTHETIC HYDROCARBON TYPE, GRADE JP-10 METRIC 28-December-2006 SUPERSEDING MIL-P-87107C 21 February 1989 DETAIL SPECIFICATION PROPELLANT, HIGH DENSITY SYNTHETIC HYDROCARBON TYPE, GRADE JP-10 This specification is approved for use by all Departments

More information

COMMERCIAL ITEM DESCRIPTION BEARING, BALL, ANNULAR, SINGLE ROW, RADIAL, NON-FILLING SLOT, DIMENSION SERIES 03

COMMERCIAL ITEM DESCRIPTION BEARING, BALL, ANNULAR, SINGLE ROW, RADIAL, NON-FILLING SLOT, DIMENSION SERIES 03 METRIC A-A-59585C 15 September 2008 SUPERSEDING A-A-59585B 23 September 2003 COMMERCIAL ITEM DESCRIPTION BEARING, BALL, ANNULAR, SINGLE ROW, RADIAL, NON-FILLING SLOT, DIMENSION SERIES 03 The General Services

More information

PERFORMANCE SPECIFICATION CLEANING COMPOUND, DEGREASING AND DEPRESERVING SOLVENT

PERFORMANCE SPECIFICATION CLEANING COMPOUND, DEGREASING AND DEPRESERVING SOLVENT NOT MEASUREMENT SENSITIVE MIL-PRF-11090J 18 October 2011 SUPERSEDING MIL-PRF-11090H w/amendment 1 19 May 2006 PERFORMANCE SPECIFICATION CLEANING COMPOUND, DEGREASING AND DEPRESERVING SOLVENT This specification

More information

DETAIL SPECIFICATION SHEET SLEEVE, SWAGING-WIRE ROPE

DETAIL SPECIFICATION SHEET SLEEVE, SWAGING-WIRE ROPE INCH-POUND 3 December 2012 SUPERSEDING 30 September 2011 DETAIL SPECIFICATION SHEET SLEEVE, SWAGING-WIRE ROPE This specification is approved for use by all Departments and Agencies of the Department of

More information

[INCH-POUND] A-A December 1999 SUPERSEDING MIL-C-4109F 31 October 1986

[INCH-POUND] A-A December 1999 SUPERSEDING MIL-C-4109F 31 October 1986 [INCH-POUND] 30 December 1999 SUPERSEDING MIL-C-4109F 31 October 1986 COMMERCIAL ITEM DESCRIPTION COUPLING HALVES, QUICK-DISCONNECT The General Services Administration has authorized the use of this commercial

More information

MILITARY SPECIFICATION MICROCIRCUITS, DIGITAL, BIPOLAR, ADVANCED LOW POWER SCHOTTKY TTL, NAND GATES, MONOLITHIC SILICON

MILITARY SPECIFICATION MICROCIRCUITS, DIGITAL, BIPOLAR, ADVANCED LOW POWER SCHOTTKY TTL, NAND GATES, MONOLITHIC SILICON INCH-POUND MIL-M-38510/370A 15 July 2004 SUPERSEDING MIL-M-38510/370(USAF) 18 March 1983 MILITARY SPECIFICATION MICROCIRCUITS, DIGITAL, BIPOLAR, ADVANCED LOW POWER SCHOTTKY TTL, NAND GATES, MONOLITHIC

More information

PERFORMANCE SPECIFICATION SHEET SWITCHES, SENSITIVE, 10 AMPERES AND LOW LEVEL, UNSEALED

PERFORMANCE SPECIFICATION SHEET SWITCHES, SENSITIVE, 10 AMPERES AND LOW LEVEL, UNSEALED INCH-POUND 2 January 201 SUPERSEDING 1 May 200 PERFORMANCE SPECIFICATION SHEET SWITCHES, SENSITIVE, AMPERES AND LOW LEVEL, UNSEALED This specification is approved for use by all Departments and Agencies

More information

PERFORMANCE SPECIFICATION SHEET

PERFORMANCE SPECIFICATION SHEET INCH-POUND MIL-PRF-24236/24E 5 April 2006 SUPERSEDING MIL-PRF-24236/24D 22 January 2001 PERFORMANCE SPECIFICATION SHEET SWITCHES, THERMOSTATIC, (BIMETALLIC), SUBMINIATURE, TYPE I, HERMETICALLY SEALED,

More information

Tests conducted under the following industry standards for PermaFrost API ASHRAE ARI ASTM EPA ANSI UL. SINCE 1985 Quality Controlled Through Analysis

Tests conducted under the following industry standards for PermaFrost API ASHRAE ARI ASTM EPA ANSI UL. SINCE 1985 Quality Controlled Through Analysis Tests conducted under the following industry standards for PermaFrost API ASHRAE ARI ASTM EPA ANSI UL SINCE 1985 Client: Powertron LLC Requested By: Mr. Tony Sgarbi Sample: 10% PermaFrost + 90% Report

More information

PROCUREMENT SPECIFICATION FOR CNP19 CHERRY RIVETLESS NUT PLATE

PROCUREMENT SPECIFICATION FOR CNP19 CHERRY RIVETLESS NUT PLATE PROCUREMENT SPECIFICATION NUMBER PRINTED COPIES OF THIS DOCUMENT ARE CONSIDERED REFERENCE UNLESS OTHERWISE STAMPED IN RED INK. PROCUREMENT SPECIFICATION FOR CNP19 CHERRY RIVETLESS NUT PLATE Authorizing

More information

DMS-9202 Asphaltic Concrete Patching Material (Stockpile Storage or Bagged)

DMS-9202 Asphaltic Concrete Patching Material (Stockpile Storage or Bagged) Asphaltic Concrete Patching Material (Stockpile Storage or Bagged) Effective Date: May 2017 1. DESCRIPTION This Specification governs for crushed stone asphaltic concrete intended primarily as a cool-

More information

REVISIONS SYMBOL DESCRIPTION DATE APPROVAL

REVISIONS SYMBOL DESCRIPTION DATE APPROVAL REVISIONS SYMBOL DESCRIPTION DATE APPROVAL L Revised per RN A-203. 2/23/16 JS K Revised per RN A-191 12/29/14 JS J Revised per RN A-183 4/25/13 JS I Revised per RN A-170. 7/15/11 JS H Revised per RN A-151.

More information

MATERIAL SPECIFICATION FOR ORGANIC SOLVENT BASED TRAFFIC PAINT

MATERIAL SPECIFICATION FOR ORGANIC SOLVENT BASED TRAFFIC PAINT ONTARIO PROVINCIAL STANDARD SPECIFICATION METRIC OPSS 1712 FEBRUARY 1991 MATERIAL SPECIFICATION FOR ORGANIC SOLVENT BASED TRAFFIC PAINT 1712.01 SCOPE 1712.02 REFERENCES 1712.03 DEFINITIONS 1712.05 MATERIALS

More information

Report On Sequence IVB Evaluation Version. Conducted For. NR = Non-reference oil test RO = Reference oil test

Report On Sequence IVB Evaluation Version. Conducted For. NR = Non-reference oil test RO = Reference oil test Report On Evaluation Version Conducted For V = Valid I = Invalid N = Results cannot be interpreted as representative of oil performance (Nonreference oil) and shall not be used for multiple test acceptance

More information

PERFORMANCE SPECIFICATION SHEET RUBBER, SYNTHETIC, TUBING

PERFORMANCE SPECIFICATION SHEET RUBBER, SYNTHETIC, TUBING INCH-POUND 15 June 2009 SUPERSEDING MIL-R-6855/4 16 February 1987 PERFORMANCE SPECIFICATION SHEET RUBBER, SYNTHETIC, TUBING This specification is approved for use by all Departments and Agencies of the

More information

Genuine Aircraft Hardware Co. MIL H 6000 B It is for push on and clamp applications.

Genuine Aircraft Hardware Co. MIL H 6000 B It is for push on and clamp applications. Genuine Aircraft Hardware Co. MIL H 6000 B This oil-resistant tube is reinforced with a high strength, mildew-resistant yarn designed to withstand oil, alcohol, coolant, fuel, water and temperatures from

More information

INCH-POUND. MIL-PRF-46103E 6 January 1998 SUPERSEDING MIL-A-46103D 23 June l989 PERFORMANCE SPECIFICATION ARMOR: LIGHTWEIGHT, COMPOSITE

INCH-POUND. MIL-PRF-46103E 6 January 1998 SUPERSEDING MIL-A-46103D 23 June l989 PERFORMANCE SPECIFICATION ARMOR: LIGHTWEIGHT, COMPOSITE INCH-POUND MIL-PRF-46103E 6 January 1998 SUPERSEDING MIL-A-46103D 23 June l989 PERFORMANCE SPECIFICATION ARMOR: LIGHTWEIGHT, COMPOSITE This specification is approved for use by all Departments and Agencies

More information

Specifications for Refrigerants

Specifications for Refrigerants AHRI Standard 700 with Addendum 1 2016 Standard for Specifications for Refrigerants WITH ADDENDUM 1, SPECIFICATIONS FOR REFRIGERANTS September 2016 Addendum 1 (dated September 2016) of AHRI Standard 700-2016,

More information

DETAIL SPECIFICATION SHEET SLEEVE, SWAGING-WIRE ROPE

DETAIL SPECIFICATION SHEET SLEEVE, SWAGING-WIRE ROPE INCH-POUND 30 September 2011 SUPERSEDING MS51844D 19 April 2007 DETAIL SPECIFICATION SHEET SLEEVE, SWAGING-WIRE ROPE This specification is approved for use by all Departments and Agencies of the Department

More information

COMPETITIVE INITIATIVE AVIATION FUEL RECLAMATION SYSTEM TECHNICAL SPECIFICATION

COMPETITIVE INITIATIVE AVIATION FUEL RECLAMATION SYSTEM TECHNICAL SPECIFICATION 1.0 SCOPE COMPETITIVE INITIATIVE AVIATION FUEL RECLAMATION SYSTEM TECHNICAL SPECIFICATION A system brand name or equal to Filterdyne Filtration Systems, Inc. Fuel Reclaim System Model F-111 Special, as

More information

DETAIL SPECIFICATION SHEET SWITCHES, TOGGLE, MINIATURE, LEVER SEAL, PANEL SEAL, FOUR POLE LOGIC LOAD TO 5 AMPERES

DETAIL SPECIFICATION SHEET SWITCHES, TOGGLE, MINIATURE, LEVER SEAL, PANEL SEAL, FOUR POLE LOGIC LOAD TO 5 AMPERES INCH-POUND MIL-DTL-83731/1B July 010 SUPERSEDING MIL-S-83731/1A 0 March 1987 DETAIL SPECIFICATI SHEET SWITCHES, TOGGLE, MINIATURE, LEVER SEAL, PANEL SEAL, FOUR POLE LOGIC LOAD TO 5 AMPERES Inactive for

More information

COMMERCIAL ITEM DESCRIPTION CLAMPS, HOSE

COMMERCIAL ITEM DESCRIPTION CLAMPS, HOSE INCH-POUND 7 JUNE 2006 SUPERSEDING A-A-52506B 16 AUGUST 1996 COMMERCIAL ITEM DESCRIPTION CLAMPS, HOSE The General Services Administration has authorized the use of this Commercial Item Description (CID)

More information

DETAIL SPECIFICATION SHEET NUT, TUBE COUPLING, SHORT

DETAIL SPECIFICATION SHEET NUT, TUBE COUPLING, SHORT INCH-POUND 19 August 2014 SUPERSEDING w/amendment 1 23 January 2013 DETAIL SPECIFICATION SHEET NUT, TUBE COUPLING, SHORT This specification is approved for use by all Departments and Agencies of the Department

More information

TMS CABLE MARKERS CM-SCE & CM-SCE-TP. Tie on Identification Product

TMS CABLE MARKERS CM-SCE & CM-SCE-TP. Tie on Identification Product Page 1 of 12 October 2015 Specification RW-2513 Document Number: 108-121016 TMS CABLE MARKERS CM-SCE & CM-SCE-TP Including HL cable marker range Tie on Identification Product SCOPE This quality assurance

More information

DEFENSE LOGISTICS AGENCY LAND AND MARITIME P.O. BOX 3990 COLUMBUS, OH

DEFENSE LOGISTICS AGENCY LAND AND MARITIME P.O. BOX 3990 COLUMBUS, OH DEFENSE LOGISTICS AGENCY LAND AND MARITIME P.O. BOX 3990 COLUMBUS, OH 43218-3990 July 26, 2018 MEMORANDUM FOR MILITARY/INDUSTRY DISTRIBUTION SUBJECT: Initial draft of MIL-STD-1560 w/change 2 (see table

More information

PERFORMANCE SPECIFICATION SHEET BATTERY, RECHARGEABLE, NICKEL CADMIUM, VENTED, 1.2-VOLT, 13 AMPERE- HOUR, BB-475/A CELL

PERFORMANCE SPECIFICATION SHEET BATTERY, RECHARGEABLE, NICKEL CADMIUM, VENTED, 1.2-VOLT, 13 AMPERE- HOUR, BB-475/A CELL INCH-POUND 25 FEB 2011 PERFORMANCE SPECIFICATION SHEET BATTERY, RECHARGEABLE, NICKEL CADMIUM, VENTED, 1.2-VOLT, 13 AMPERE- HOUR, BB-475/A CELL This specification is approved for use within Army CECOM Life

More information

PERFORMANCE SPECIFICATION MRCRA3T AND INSTRUMENT, FUEL AND OXIDIZER RESKTANT

PERFORMANCE SPECIFICATION MRCRA3T AND INSTRUMENT, FUEL AND OXIDIZER RESKTANT IW3LPRF27617F 17 Februam 199S SUPERSEDING fw32.gn6l7e IS ApsU 1994 PERFORMANCE SPECIFICATION GM MRCRA3T AND INSTRUMENT, FUEL AND OXIDIZER RESKTANT flsis spilicmion isspprovcdfixw by alldcpmmems md Agencies

More information

PERFORMANCE SPECIFICATION LUBRICATING OIL, INTERNAL COMBUSTION ENGINE, PRESERVATIVE BREAK-IN

PERFORMANCE SPECIFICATION LUBRICATING OIL, INTERNAL COMBUSTION ENGINE, PRESERVATIVE BREAK-IN NOT-MEASUREMENT SENSITIVE 31 July 1998 SUPERSEDING MIL-L-21260D 29 April 1988 PERFORMANCE SPECIFICATION LUBRICATING OIL, INTERNAL COMBUSTION ENGINE, PRESERVATIVE BREAK-IN This specification is approved

More information

MIL-STD S 26 JULY 1985

MIL-STD S 26 JULY 1985 k -. Downloaded from http://www.everyspec.com -- MIL-STD-3-S 6 JULY 985 SUPERSEDING MIL-STD-3(ln 3 MAY 967 part) MILITARY STANDARD FASTENER TEST METHODS METHOD 5, DRIVING RECESS TORQUE QUALITY CONFORMANCE

More information

SECTION 916 (Pages ) is deleted and the following substituted: SECTION 916 BITUMINOUS MATERIALS

SECTION 916 (Pages ) is deleted and the following substituted: SECTION 916 BITUMINOUS MATERIALS 916 BITUMINOUS MATERIALS. (REV 7-28-03) (FA 1-13-04) (7-04) SECTION 916 (Pages 785-797) is deleted and the following substituted: SECTION 916 BITUMINOUS MATERIALS 916-1 Superpave PG Asphalt Binder: 916-1.1

More information

DETAIL SPECIFICATION FASTENER ELEMENT, SELF-LOCKING, THREADED FASTENER, 250 F MAXIMUM

DETAIL SPECIFICATION FASTENER ELEMENT, SELF-LOCKING, THREADED FASTENER, 250 F MAXIMUM INCH-POUND 2 JUNE 1997 SUPERSEDING MIL-F-18240E 1 DECEMBER 1989 DETAIL SPECIFICATION FASTENER ELEMENT, SELF-LOCKING, THREADED FASTENER, 250 F MAXIMUM This specification is approved for use by all Departments

More information

Explanatory sheet about safety of product for transportation (Safety Data Sheet for transportation) 1. Basic item 2. Product information

Explanatory sheet about safety of product for transportation (Safety Data Sheet for transportation) 1. Basic item 2. Product information Issued/Revised date :June 14 2018 Document No. : LE-180614006 Explanatory sheet about safety of product for transportation (Safety Data Sheet for transportation) 1. Basic item Product name Lithium-Ion

More information